发明名称 Simplified anti-vibration suspension for helicopter rotor
摘要 The anti-vibration suspension comprises three inclined bars (8) each articulated (9,11) on the structure (1) and the on the transmission box (2) by a rigid lever (12). The lever which supports a swinging mass (13) is pivoted on the transmission box. For each inclined bar a traction bar (16) is also articulated (17,18) on the structure and the transmission box. The corresponding lever is articulated on the box by pivoting on the upper end part of the corresponding traction bar.
申请公布号 FR2777860(A1) 申请公布日期 1999.10.29
申请号 FR19980005093 申请日期 1998.04.23
申请人 EUROCOPTER FRANCE 发明人 CERTAIN NICOLAS PIERRE GEORGES
分类号 B64C27/00;(IPC1-7):B64C27/00;F16F7/10;F16F15/04;F16F15/28 主分类号 B64C27/00
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